On rearrangement invariant hull of generalized Sobolev spaces from the Sobolev
space ẆE m(Ω), where m ∈ N, Ω is an open bounded domain in Rn, and E = E(Ω) is a
Elastic-Plastic Analysis of Space Trusses with Large Displacements the ultimate load of
space trusses with large displacements. A direct
method is treated in this investigation
Attractor property for terminal manifold in control synthesis problem function depending on the
state space vector. After substituting to the system of ordinary differential
Control synthesis by network operator method for spacecraft descent on the moon. Mathematical model of the spacecraft, initial
states, and terminal conditions are given. The goal
STABILITY ANALYSIS OF SPACE TRUSSES method is presented that predicts unstable configurations (singular
states) by computing the nonlinear
Features of semantic spaces of students’ mental state image in dynamics of time spaces of a figurative level of mental representations of students’ mental
states. The following
State space method for hybrid discrete-continuous systems with controlState space method for hybrid discrete-continuous systems with control
Monitoring of illegal placement of solid waste with the use of space technology is devoted to development and use of the
space and geoinformational technologies allowing the
state